CA2742290C - Ensemble structurel d'aeronef et procede d'assemblage associe - Google Patents
Ensemble structurel d'aeronef et procede d'assemblage associe Download PDFInfo
- Publication number
- CA2742290C CA2742290C CA2742290A CA2742290A CA2742290C CA 2742290 C CA2742290 C CA 2742290C CA 2742290 A CA2742290 A CA 2742290A CA 2742290 A CA2742290 A CA 2742290A CA 2742290 C CA2742290 C CA 2742290C
- Authority
- CA
- Canada
- Prior art keywords
- wall
- structural
- composite
- slice
- passage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000000034 method Methods 0.000 title claims description 9
- 239000002131 composite material Substances 0.000 claims abstract description 153
- 230000007935 neutral effect Effects 0.000 claims description 17
- 239000000835 fiber Substances 0.000 claims description 16
- 230000006835 compression Effects 0.000 claims description 11
- 238000007906 compression Methods 0.000 claims description 11
- 210000000056 organ Anatomy 0.000 claims description 5
- 239000012530 fluid Substances 0.000 claims description 4
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 239000002184 metal Substances 0.000 abstract description 5
- 239000010410 layer Substances 0.000 description 19
- 235000012431 wafers Nutrition 0.000 description 13
- 238000005304 joining Methods 0.000 description 4
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 239000002828 fuel tank Substances 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- 230000000295 complement effect Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 230000032798 delamination Effects 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/04—Devices for fastening nuts to surfaces, e.g. sheets, plates
- F16B37/045—Devices for fastening nuts to surfaces, e.g. sheets, plates specially adapted for fastening in channels, e.g. sliding bolts, channel nuts
- F16B37/047—Barrel nuts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/02—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread
- F16B5/0291—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening members using screw-thread the threaded element being driven through the edge of a sheet plate with its axis in the plane of the plate
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
- Connection Of Plates (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1002378A FR2960852B1 (fr) | 2010-06-04 | 2010-06-04 | Ensemble structurel d'aeronef et procede d'assemblage associe |
| FR1002378 | 2010-06-04 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2742290A1 CA2742290A1 (fr) | 2011-12-04 |
| CA2742290C true CA2742290C (fr) | 2018-11-20 |
Family
ID=43446671
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2742290A Expired - Fee Related CA2742290C (fr) | 2010-06-04 | 2011-06-02 | Ensemble structurel d'aeronef et procede d'assemblage associe |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US8844869B2 (zh) |
| CN (1) | CN102310941B (zh) |
| BR (1) | BRPI1102920A2 (zh) |
| CA (1) | CA2742290C (zh) |
| FR (1) | FR2960852B1 (zh) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201105104D0 (en) * | 2011-03-28 | 2011-05-11 | Airbus Operations Ltd | Joint |
| US9452825B2 (en) * | 2013-04-19 | 2016-09-27 | The Boeing Company | Winglet attach fitting for attaching a split winglet to a wing |
| US20150000086A1 (en) * | 2013-06-28 | 2015-01-01 | GM Global Technology Operations LLC | Vehicle substrate having a pocket for isolating a fastener |
| US9896190B1 (en) * | 2014-05-07 | 2018-02-20 | The Boeing Company | Wing leading edge architecture suitable for laminar flow |
| GB201410058D0 (en) * | 2014-06-06 | 2014-07-16 | Rolls Royce Plc | A casing assembly |
| US10087970B2 (en) * | 2016-04-29 | 2018-10-02 | The Boeing Company | Sealant Containment Assembly |
| US10450053B2 (en) * | 2016-05-11 | 2019-10-22 | The Boeing Company | Methods using predictive shimming to optimize part-to-part alignment |
| EP3281869B1 (en) | 2016-08-11 | 2019-04-17 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A control system for controlling at least collective pitch of rotor blades of a multi-blade rotor in a rotary-wing aircraft |
| CN118457967A (zh) * | 2018-12-28 | 2024-08-09 | 深圳市道通智能航空技术股份有限公司 | 一种无人飞行器及其机翼组件 |
| US11038334B2 (en) | 2019-01-14 | 2021-06-15 | The Boeing Company | Aircraft wing composite ribs having electrical grounding paths |
| US10913548B2 (en) * | 2019-01-14 | 2021-02-09 | The Boeing Company | Metallic fittings for coupling composite ribs to skin panels of aircraft wings |
| US11306762B2 (en) * | 2019-07-09 | 2022-04-19 | Rohr, Inc. | Barrel nut retainer from one-way installation guide |
| CN211618061U (zh) | 2019-09-05 | 2020-10-02 | 深圳市道通智能航空技术有限公司 | 机翼拆卸组件和飞行器 |
| US11084085B1 (en) | 2020-10-23 | 2021-08-10 | Ford Global Technologies, Llc | Vehicle component joining method |
| CN114162341B (zh) * | 2021-12-17 | 2023-08-04 | 日照职业技术学院 | 一种可调式无人机摄影测量安装平台 |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2747638A (en) * | 1950-12-23 | 1956-05-29 | Emanuel L Cederquist | Bolt with locking and retaining means |
| DE3113079C2 (de) * | 1981-04-01 | 1985-11-21 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Aerodynamischer Groß-Flügel und Verfahren zu dessen Herstellung |
| GB2305226B (en) * | 1993-12-23 | 1997-07-16 | Titus Int Plc | Joint forming device |
| US5647174A (en) * | 1994-08-29 | 1997-07-15 | Mattarelli; Anthony | Collapsible mantel assembly |
| EP0810377A1 (de) * | 1996-05-28 | 1997-12-03 | Andreas Mangold | Schraubverbindung zum Verbinden von zwei Profilen |
| FR2821129B1 (fr) * | 2001-02-22 | 2003-05-16 | Eads Airbus Sa | Dispositif d'assemblage d'un panneau et d'une structure, apte a transmettre des efforts importants |
| US7658348B1 (en) * | 2005-05-23 | 2010-02-09 | Braly George W | Enhancement and extension of structural integrity of aircraft structure |
| WO2009130687A2 (en) * | 2008-04-25 | 2009-10-29 | Jose Teixeira Mao-Cheia | Balustrade |
-
2010
- 2010-06-04 FR FR1002378A patent/FR2960852B1/fr not_active Expired - Fee Related
-
2011
- 2011-06-02 CA CA2742290A patent/CA2742290C/fr not_active Expired - Fee Related
- 2011-06-03 BR BRPI1102920-0A patent/BRPI1102920A2/pt not_active Application Discontinuation
- 2011-06-03 US US13/153,050 patent/US8844869B2/en not_active Expired - Fee Related
- 2011-06-03 CN CN201110153610.1A patent/CN102310941B/zh not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US20110315820A1 (en) | 2011-12-29 |
| FR2960852A1 (fr) | 2011-12-09 |
| CN102310941B (zh) | 2015-08-19 |
| FR2960852B1 (fr) | 2013-04-12 |
| CN102310941A (zh) | 2012-01-11 |
| BRPI1102920A2 (pt) | 2013-05-14 |
| CA2742290A1 (fr) | 2011-12-04 |
| US8844869B2 (en) | 2014-09-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2742290C (fr) | Ensemble structurel d'aeronef et procede d'assemblage associe | |
| CA2623240C (fr) | Dispositif pour la fixation d'un panneau leger sur un support | |
| CA2773532C (fr) | Radome et dispositif de fixation de ce radome a un aeronef | |
| CA2781777C (fr) | Aeronef comportant une cloison interne | |
| FR2948099A1 (fr) | Procede de fabrication d'un aeronef a voilure fixe | |
| EP3505439B1 (fr) | Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure par des attaches presentant un encombrement reduit dans la zone de bord d'attaque | |
| FR2911112A1 (fr) | Section de fuselage pour aeronef et aeronef comprenant une telle section | |
| CA2702908A1 (fr) | Structure d'avion comportant des jonctions d'arrets de raidisseurs | |
| FR2927686A1 (fr) | Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef. | |
| FR2953158A1 (fr) | Procede pour realiser une jonction etanche entre des pieces d'aeronef | |
| EP3505448B1 (fr) | Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure par des attaches presentant un encombrement reduit dans la zone de bord d'attaque | |
| EP2271850B1 (fr) | Procédé d'assemblage entre une pièce en matériau métallique et une pièce en matériau composite | |
| EP3802314B1 (fr) | Porte de cabine pressurisée d'aéronef à structure formée de poutres | |
| EP3674204A1 (fr) | Voilure d'aeronef comprenant deux ailes fixees l'une sur l'autre | |
| EP3476740B1 (fr) | Structure primaire de mât de support d'un groupe propulseur d'aéronef en caisson formée par assemblage de deux demi-coquilles | |
| EP3489147A1 (fr) | Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure par des attaches partiellement enterrees dans la structure primaire | |
| FR3032905A1 (fr) | Panneau composite muni d'une terminaison d'assemblage perfectionnee et structure comportant un tel panneau | |
| FR3099464A1 (fr) | Mat reacteur pour coupler un turboreacteur a une aile d’un aeronef | |
| FR3086269A1 (fr) | Systeme de fixation d'elements d'amenagement sur un plancher de vehicule comprenant des panneaux a parois laterales perforees | |
| EP3521173A1 (fr) | Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure a l'aide d'une liaison boulonnee | |
| EP3934978B1 (fr) | Porte de cabine pressurisée d'aéronef à armature intérieure de reprise d'efforts | |
| EP4147966B1 (fr) | Aéronef comprenant une case de train d'atterrissage principale présentant une coque réalisée d'un seul tenant | |
| EP2671665A1 (fr) | Elément structurel de protection pour un véhicule, véhicule comprenant un tel élément, et procédé de réalisation | |
| EP3037684A1 (fr) | Chape avec empochement et/ou relief | |
| FR3026151A1 (fr) | Dispositif d'assemblage a ecrou-barillet, ensemble structurel d'aeronef comprenant un tel dispositif, et procede d'assemblage correspondant |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request |
Effective date: 20160509 |
|
| MKLA | Lapsed |
Effective date: 20220301 |
|
| MKLA | Lapsed |
Effective date: 20200831 |